Propulsion and Power Plants
Аuthors
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
e-mail: agulnik@mai.ru
Abstract
The summary: results settlement, experimental researches of backlashes on EFFICIENCY of axial turbine stages Are resulted, the method of the account of losses from a radial backlash when losses basically are defined by size of leak of a working body through a radial backlash is given. Comparison of an offered method with known of the literature and with the spent experiments is spent. Accuracy of calculation is raised.Keywords:
axial turbine stages, consumption coefficients, clearances.
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